Structural Acoustic Prediction and Interior Noise Control Technology

By National Aeronautics and Space Administration

This report documents the results of Task 14, "Structural Acoustic Prediction and Interior Noise Control Technology." The task was to evaluate the performance of tuned foam elements (termed Smart Foam) both analytically and experimentally. Results taken from a three-dimensional finite element model of an active, tuned foam element are presented. Measurements of sound absorption and sound transmission loss were taken using the model. These results agree well with published data. Experimental performance data were taken in Boeing's Interior Noise Test Facility where 12 smart foam elements were applied to a 757 sidewall. Several configurations were tested. Noise reductions of 5-10 dB were achieved over the 200-800 Hz bandwidth of the controller. Accelerometers mounted on the panel provided a good reference for the controller. Configurations with far-field error microphones outperformed near-field cases.Mathur, G. P. and Chin, C. L. and Simpson, M. A. and Lee, J. T. and Palumbo, Daniel L. (Technical Monitor)Langley Research CenterAIRCRAFT NOISE; ACOUSTIC ATTENUATION; MATHEMATICAL MODELS; TECHNOLOGY UTILIZATION; CONTROLLERS; AIRCRAFT STRUCTURES; NOISE REDUCTION; ACCELEROMETERS; FLIGHT TESTS; FUSELAGES; SOUND TRANSMISSION; FINITE ELEMENT METHOD

• Format: Paperback
• Language: English
• ISBN: 1723890006
• ISBN13: 9781723890000
• Release Date: January 1
• Publisher: Independently Published
• Length: 50 Pages
• Weight: 0.31 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"